NTSB CAROL · Event
Event CEN12LA675
Registry · N7133N
FAA Aircraft Registry record.
Make / Model
BEECH E33
Year of manufacture
1968 · 44 years old at event
Engine
CONT MOTOR I0-470 SERIES (260 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19680109
ADS-B equipped
Yes — Mode-S A98A00
Registrant of record
WEIGAND JEFFREY DAVID JR
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The loss of engine power for reasons that could not be determined during postaccident examinations and testing.
Factual narrative
On September 26, 2012, approximately 1500 mountain daylight time, a Beech E33, N7133N, registered to All Seasons Window Cleaning LLC, of Broomfield, Colorado, sustained substantial damage during a forced landing after a loss of engine power shortly after takeoff from the Greeley-Weld County Airport, Greeley, Colorado. The commercial pilot, who was the sole occupant, was not injured. Visual meteorological conditions prevailed and a flight plan was not filed. The local flight was being conducted under the provisions of 14 Code of Federal Regulations Part 91. On the morning of the flight, the pilot/owner asked a local A&P mechanic to take a look at airplane's fuel system. The mechanic opened the engine cowling and found nothing out-of-the-normal visually. He then disconnected the fuel line between the fuel pump and the throttle body, unmetered fuel, and installed a remote pressure gauge to check to see where the fuel pressure was set. After removing the right side inspection cover of the lower cowling to access the throttle body, and while the pilot operated the engine from the cockpit controls, he found that the idle mixture was slightly rich and the fuel pressure at idle was within specifications. He readjusted the idle mixture setting at the throttle body and then checked the fuel pressure which was within specifications. The engine was shut down twice, restarted and the fuel pressure at idle and idle mixture settings were checked again. The pilot said that the engine ran so much better after making the idle mixture adjustments. After making final checks for fuel pressure and the locknuts on the idle mixture arm and an overall visual check of the engine compartment, the cowls were reinstalled. After a normal run-up, the pilot took off from runway 9 for a local test flight. The airplane was seen climbing out normally and started to circle the airport. The airplane then descended toward the approach end of runway 27 as the pilot declared an emergency due to engine problems. The airplane landed in plowed field gear up about 1/2 mile from the approach end of runway 27. After the accident, the airplane was moved to a local facility for further examination. FAA inspectors examined the wreckage and could not determine the cause of the loss of engine power. An engine run was attempted on January 3, 2013, at Beegles Aircraft in Greeley, CO. The engine was run on the airframe with a different, unbent slave propeller and taken through a series of tests up to full power. No anomalies were noted with the exception of slight fuel flow indicator fluctuations. There was nothing found that may have contributed attributed to the reported loss of power by the pilot. Before the flight, a mechanic assisted the pilot with adjusting the engine mixture settings during several engine starts and run-ups. The pilot was satisfied with the adjustments and proceeded with the local test flight. Witnesses reported observing the airplane climb out normally and then start to circle the airport. The airplane then descended toward the airport as the pilot declared an emergency due to engine problems. The pilot landed the airplane in a plowed field with the gear up, which resulted in substantial damage to the airplane. Postaccident examination of the engine did not reveal any anomalies that may have contributed to the reported loss of power. Additionally, the slave propeller was replaced, and the engine was test run on the airframe up to full power with no anomalies noted except for slight fuel flow indicator fluctuations. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- C Not determined-Not determined-(general)-(general)-Unknown/Not determined - C
Verbatim from NTSB's published report. Source file
NTSB_2012_CEN12LA675.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (stall). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- NASA NTRS 2026 · Conference Paper
Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- arXiv 2023 · arXiv preprint
Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- arXiv 2023 · arXiv preprint
Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2023 · arXiv preprint
Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
- arXiv 2022 · arXiv preprint
Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER)
Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…
Browse the full corpus — academia portal ↗